Vacuum pumps

Information

  • Patent Grant
  • 6709228
  • Patent Number
    6,709,228
  • Date Filed
    Tuesday, October 15, 2002
    22 years ago
  • Date Issued
    Tuesday, March 23, 2004
    20 years ago
Abstract
A compound vacuum pump comprising at least one turbo-molecular stage and downstream therefrom a multi-channel molecular drag stage, a first inlet through which fluid can pass through the turbo-molecular stage and the molecular drag stage towards a pump outlet, a second inlet through which fluid can enter the pump at a location between the turbo-molecular and the molecular drag stages to pass only through the molecular drag stage towards the pump outlet, in which one or more channels of the molecular drag stage are adapted to communicate directly with the second inlet whilst the remaining channel or channels communicate with the turbo-molecular stage.
Description




FIELD OF THE INVENTION




This invention relates to vacuum pumps and in particular to compound vacuum pumps which employ at least one turbo-molecular stage and one molecular drag stage.




BACKGROUND OF THE INVENTION




There is described in European patent publication number 0 919 726 a vacuum pump comprising first and second turbo-molecular stages and a molecular drag (Holweck) stage. This known pump has a first inlet through which fluid being pumped passes through all the pump stages and a second inlet through which fluid enters the pump between the two turbo-molecular stages and passes only through one turbo-molecular stage and the Holweck stage. The turbo-molecular stage upstream of the second inlet is sized differently from the turbo-molecular stage downstream of the second inlet so that the vacuum pump suits the pressure requirements or pumping capacities of the chambers/systems being evacuated and attached to the first and second inlets respectively.




This known “split flow” turbo-molecular pump facilitates the differential pumping of, for example, two chambers of a scientific instrument. For example, in well known types of mass spectrometer that part of the apparatus known as the detector commonly has to be operated at, for example, 10


−6


mbar whereas that part known as the analyser has to be operated at a different level of vacuum for example 10


−3


mbar. The chamber requiring the lower pressure (higher vacuum) is attached to the first inlet so that the fluid being evacuated is subject to all the stages of the pump whilst the chamber requiring the higher pressure (lower vacuum) is attached to the second inlet so that the fluid being evacuated is subject only to the pump stages downstream of the second inlet.




With liquid phase mass spectrometer (MS) systems there is increasingly a demand for higher gas loads to be consumed by the vacuum system. The highest gas load handling capacity is required at the comparatively “high” pressure end of the pump. As the gas load diminishes in the subsequent chambers so to the system pressure decreases until eventually it reaches a level acceptable for analysis.




OBJECTS OF THE INVENTION




It is an aim of the present invention to provide an improved compound vacuum pump including at least one turbo-molecular stage and downstream therefrom a multi-channel molecular drag stage in which one or more channels of the molecular drag stage are devoted to pumping a high pressure fluid inlet whilst the remainder of the channels are devoted to “back” the turbo-molecular stage.




SUMMARY OF THE INVENTION




According to the present invention, a compound vacuum pump comprises at least one turbo-molecular stage and downstream therefrom a multi-channel molecular drag stage, a first inlet through which fluid can pass through the turbo-molecular stage and the molecular drag stage towards a pump outlet, a second inlet through which fluid can enter the pump at a location between the turbo-molecular and the molecular drag stages to pass only through the molecular drag stage towards the pump outlet, in which one or more channels of the molecular drag stage are adapted to communicate directly with the second inlet whilst the remaining channel or channels communicate with the turbo-molecular stage.




Preferably, the multi-channel molecular drag stage is a Holweck stage with a plurality of channels arranged as a plurality of helixes.




In one embodiment, a baffle directs one or more of the helical channels of the Holweck stage towards the second inlet.











BRIEF DESCRIPTION OF THE DRAWINGS




An embodiment of the invention will now be described, by way of example, reference being made to the Figures of the accompanying diagrammatic drawings in which:





FIG. 1

is a vertical cross-section through a known compound vacuum pump employing two turbo-molecular stages, a Holweck stage, a low pressure inlet and a high pressure inlet;





FIG. 2

is a vertical cross-section through a compound vacuum pump according to the present invention;





FIG. 3

is a cross section on the line X—X of

FIG. 2

;





FIG. 4

is an enlarged detail of the compound vacuum pump of

FIGS. 2 and 3

at a high pressure inlet interstage between a turbo-molecular stage and a Holweck stage;





FIG. 5

is a detail in perspective of the Holweck stage and a baffle member forming part of the compound vacuum pump of

FIG. 2

; and





FIG. 6

is a schematic illustration of an embodiment of the invention in which a single channel of the Holweck stage is directed to communicate directly with a high pressure fluid inlet whilst the remaining four channels communicate with a turbo-molecular stage.











DETAILED DESCRIPTION OF THE INVENTION




Referring first to

FIG. 1

there is shown a known compound vacuum pump having a multi-component body


1


within which is mounted a shaft


2


. Rotation of the shaft


2


is effected by a motor


3


positioned about the shaft


2


. The shaft


2


is mounted in lower and upper bearings


4


,


5


respectively.




The pump includes two sets of turbo-molecular stages


6


,


7


. The first set of turbo-molecular stages


6


comprises four rotor and stator blade pairs of known angled construction, a rotor blade stage is indicated at


8


and a stator blade stage is indicated at


9


.




The second set of turbo-molecular stages


7


comprises a further six rotor and stator blade pairs of angled construction, a rotor blade stage is indicated at


12


and a stator blade stage is indicated at


13


in the drawing.




The pump is provided with a low pressure inlet


10


and a higher pressure inlet


16


.




Downstream of the turbo-molecular stage


7


are a number of Holweck stages. These Holweck stages comprise two rotating cylinders


17


,


18


and corresponding annular stators


19


,


20


having helical channels formed therein all in a manner known per se. Downstream of the Holweck stages is a pump outlet


22


.




In this known pump, the inlet


10


is connected to a chamber/system requiring a relatively high vacuum (low pressure) and the fluid pumped through the inlet


10


passes through both the turbo stages


6


,


7


and also the Holweck stages and exits the pump via the outlet


22


. The inlet


16


is connected to a chamber/system requiring less vacuum (higher pressure) and the fluid pumped through the inlet


16


passes only through the turbo-molecular stages


7


and the Holweck stages and exits the pump via the outlet


22


.




Referring now to

FIGS. 2

to


4


where like reference numerals denote like parts, a compound vacuum pump


30


comprises a body


1


within which is mounted a vertical shaft


2


supported by lower and upper bearings


4


,


5


. Rotation of the shaft


2


is effected by a motor


3


.




The pump


30


has two sets of turbo-molecular stages


6


,


7


and a Holweck stage


32


.




The pump


30


has three inlets and an outlet


22


. The first inlet


34


(mid gas pressure) is located interstage the two turbo-molecular stages


6


,


7


; the second inlet


36


(high gas pressure) is located interstage the turbo-molecular stage


7


and the Holweck stage


32


; and the third inlet


38


(low gas pressure) is located upstream of all three stages




The Holweck stage


32


includes two rotating cylinders


17


,


18


and corresponding annular stators


19


,


20


and helical channels formed thereon all in a manner known per se.




According to the invention, and as shown in

FIG. 6

, one or more channels of the Holweck stage


32


is adapted to communicate directly with the high pressure inlet


36


whilst the remaining channel or channels communicate and serve to back turbo-molecular stage


7


.




Referring also to

FIG. 5

, the Holweck stage


32


is provided with a baffle member


40


having a radially inwardly directed flange


42


which allows only one channel (as shown) of the Holweck stage to communicate with the high pressure gas inlet


36


and prevents back streaming of the high pressure gas in to the turbo blades of the turbo-molecular stage


7


.




The remaining channels of the Holweck stage are used to “back” the turbo blade stages of the turbo-molecular stage


7


.




It will be apparent that the flange


42


could be extended so that more than one channel could be directed at the high pressure gas inlet


36


.




A particular advantage of the embodiment described above is that the use of varying numbers of Holweck molecular drag stage channels for the purpose of either pumping the high pressure inlet or “back” the turbo blades stages


7


is matched to individual scientific instrument applications.



Claims
  • 1. A compound vacuum pump comprising at least one turbo-molecular stage and downstream therefrom a multi-channel molecular drag stage, a first inlet through which fluid can pass through the turbo-molecular stage and the molecular drag stage towards a pump outlet, a second inlet through which fluid can enter the pump at a location between the turbo-molecular and the molecular drag stages to pass only through the molecular drag stage towards the pump outlet, in which one or more channels of the molecular drag stage are adapted to communicate directly with the second inlet whilst the remaining channel or channels communicate with the turbo-molecular stage.
  • 2. A compound vacuum pump as claimed in claim 1 in which the multi-channel molecular drag stage is a Holweck stage with a plurality of channels arranged as a plurality of helixes.
  • 3. A compound vacuum pump as claimed in claim 2 in which a baffle directs one or more of the helical channels of the Holweck stage towards the second inlet.
  • 4. A compound vacuum pump as claimed in claim 3 in which at least two turbo-molecular stages are provided upstream of the Holweck stage.
  • 5. A compound vacuum pump as claimed in claim 4 in which the pump has at least one additional inlet through which fluid will pass through both the turbo-molecular stages and the molecular drag stage towards the outlet.
  • 6. A compound vacuum pump as claimed in claim 5 in which the baffle includes a flange for inhibiting the back streaming of fluid from the Holweck stage towards the turbo-molecular stage.
  • 7. A compound vacuum pump as claimed in claim 4 in which the baffle includes a flange for inhibiting the back streaming of fluid from the Holweck stage towards the turbo-molecular stage.
  • 8. A compound vacuum pump as claimed in claim 2 in which at least two turbo-molecular stages are provided upstream of the Holweck stage.
  • 9. A compound vacuum pump as claimed in claim 8 in which the pump has at least one additional inlet through which fluid will pass through both the turbo-molecular stages and the molecular drag stage towards the outlet.
  • 10. A compound vacuum pump as claimed in claim 9 in which the baffle includes a flange for inhibiting the back streaming of fluid from the Holweck stage towards the turbo-molecular stage.
  • 11. A compound vacuum pump as claimed in claim 8 in which the baffle includes a flange for inhibiting the back streaming of fluid from the Holweck stage towards the turbo-molecular stage.
  • 12. A compound vacuum pump as claimed in claim 3 in which the baffle includes a flange for inhibiting the back streaming of fluid from the Holweck stage towards the turbo-molecular stage.
Priority Claims (1)
Number Date Country Kind
0124731 Oct 2001 GB
US Referenced Citations (6)
Number Name Date Kind
5707213 Conrad Jan 1998 A
5733104 Conrad et al. Mar 1998 A
6030189 Bohm et al. Feb 2000 A
6193461 Hablanian Feb 2001 B1
6200107 Brewster Mar 2001 B1
6220824 Hablanian Apr 2001 B1
Foreign Referenced Citations (3)
Number Date Country
0 919 726 Jun 1999 EP
1 085 214 Mar 2001 EP
2 360 066 Sep 2001 GB
Non-Patent Literature Citations (2)
Entry
UK Patent Office Search Report dated Apr. 8, 2002.
European Search Report of Application No. EP 02 25 7066 completed Dec. 6, 2002.